Question: Consider a shock wave moving through air at 2 9 3 K and 1 atm. Immediately downstream ( behind ) the shock wave, the air

Consider a shock wave moving through air at 293 K and 1 atm. Immediately downstream (behind) the shock wave, the air temperature and pressure increase to 790 K and 9.656 atm. Calculate the changes in the following quantities across the wave (show details of your calculation):
a. Enthalpy
b. Internal energy
c. Entropy

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